A Review of Distributed Electric Propulsion Concepts for Air Vehicle Technology

H. D. Kim, Aaron T. Perry, Phillip J. Ansell
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引用次数: 185

Abstract

The emergence of distributed electric propulsion (DEP) concepts for aircraft systems has enabled new capabilities in the overall efficiency, capabilities, and robustness of future air vehicles. Distributed electric propulsion systems feature the novel approach of utilizing electrically-driven propulsors which are only connected electrically to energy sources or power-generating devices. As a result, propulsors can be placed, sized, and operated with greater flexibility to leverage the synergistic benefits of aero-propulsive coupling and provide improved performance over more traditional designs. A number of conventional aircraft concepts that utilize distributed electric propulsion have been developed, along with various short and vertical takeoff and landing platforms. Careful integration of electrically-driven propulsors for boundary-layer ingestion can allow for improved propulsive efficiency and wake-filling benefits. The placement and configuration of propulsors can also be used to mitigate the trailing vortex system of a lifting surface or leverage increases in dynamic pressure across blown surfaces for increased lift performance. Additionally, the thrust stream of distributed electric propulsors can be utilized to enable new capabilities in vehicle control, including reducing requirements for traditional control surfaces and increasing tolerance of the vehicle control system to engine-out or propulsor-out scenarios. If one or more turboelectric generators and multiple electric fans are used, the increased effective bypass ratio of the whole propulsion system can also enable lower community noise during takeoff and landing segments of flight and higher propulsive efficiency at all conditions. Furthermore, the small propulsors of a DEP system can be installed to leverage an acoustic shielding effect by the airframe, which can further reduce noise signatures. The rapid growth in flight-weight electrical systems and power architectures has provided new enabling technologies for future DEP concepts, which provide flexible operational capabilities far beyond those of current systems. While a number of integration challenges exist, DEP is a disruptive concept that can lead to unprecedented improvements in future aircraft designs.
飞行器分布式电力推进技术研究进展
飞机系统分布式电力推进(DEP)概念的出现,为未来飞行器的整体效率、性能和稳健性提供了新的能力。分布式电力推进系统的特点是利用电力驱动的推进器,这些推进器只与能源或发电设备电连接。因此,推进器可以更灵活地放置、大小和操作,以利用航空推进耦合的协同效益,并提供比传统设计更好的性能。许多利用分布式电力推进的传统飞机概念已经被开发出来,以及各种短距和垂直起降平台。仔细集成用于边界层摄取的电力驱动推进器可以提高推进效率和尾迹填充效益。推进器的位置和配置也可以用来减轻升力表面的尾涡系统,或者利用吹气表面上的动压力增加来提高升力性能。此外,分布式电动推进器的推力流可用于实现车辆控制的新功能,包括减少对传统控制面的要求,增加车辆控制系统对发动机或推进器退出场景的容忍度。如果使用一台或多台涡轮发电机和多台电风扇,整个推进系统有效涵道比的提高还可以降低飞行起降段的群体噪声,提高各种工况下的推进效率。此外,可以安装DEP系统的小型推进器,以利用机身的声屏蔽效应,从而进一步降低噪声特征。飞行重量电气系统和动力架构的快速发展为未来的DEP概念提供了新的支持技术,这些技术提供了远远超过当前系统的灵活操作能力。尽管存在许多集成挑战,但DEP是一个颠覆性的概念,可以为未来的飞机设计带来前所未有的改进。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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